2018-08-19 20:27 BST

View Issue Details Jump to Notes ]
IDProjectCategoryView StatusLast Update
0003035OpenFOAM[All Projects] Bugpublic2018-08-09 02:24
ReporterRoy 
Assigned Tohenry 
PrioritylowSeverityminorReproducibilityalways
StatusclosedResolutionfixed 
PlatformLinuxOSUbuntuOS Version16.04
Product Version6 
Target VersionFixed in Version 
Summary0003035: wrong behaviour of wingMotion tutorial using rigidBodyMotion solver
DescriptionI try to conduct the wingMotion tutorial using rigidBodyMotion solver. This tutorial employs the sixDofRigidmotion solver originally.
 
Refer to the floatingObject tutorial, the only modified file for the wingMotion tutorial is the dynamicMeshDict. Attached case is modified wingMotion tutorial using rigidBodyMotion solver. But this case crashes up after t=0.13s.

The result by paraview is also attached, which shows a continuous clockwise rotation along zAxis and results in extreme mesh deformation.
The moment of linearAxialAngularSpring is found has same direction with rotation by the output of log file, which is expected to have the adverse direction with rotation and restore the pitch motion. The rotation of paraview also show inconsistence with orientation of log file.

Does I have a wrong setup in dynamicMeshDict with rigidBodyMotion solver or miss any parameters?
TagsrigidBodyMotion
Attached Files

-Relationships
+Relationships

-Notes

~0009921

henry (manager)

User support request.
+Notes

-Issue History
Date Modified Username Field Change
2018-08-08 09:00 Roy New Issue
2018-08-08 09:00 Roy File Added: files.zip
2018-08-08 09:00 Roy Tag Attached: rigidBodyMotion
2018-08-08 09:37 henry Assigned To => henry
2018-08-08 09:37 henry Status new => closed
2018-08-08 09:37 henry Resolution open => fixed
2018-08-08 09:37 henry Note Added: 0009921
+Issue History